Systems and methods for optimizing the aimpoint for a missile

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Reexamination Certificate

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C244S003100, C244S003110, C382S100000, C382S103000, C701S001000, C701S002000, C701S003000

Reexamination Certificate

active

07968831

ABSTRACT:
Methods and systems are disclosed that automatically display an optimized aimpoint on a target image in received seeker data. In one embodiment, a method receives missile seeker target data. A seeker mode data is extracted from the received missile seeker target data. The location of a most vulnerable spot on a target is identified based on a comparison of target library data with seeker image data. A marker is generated at the location of the optimized aimpoint and output to a display.

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